UAH Archives, Special Collections, and Digital Initiatives

Browse Items (6320 total)

  • norhunorgchanorcororgcha_051608135828.pdf

    Nortronics/Northrop corporate organizational chart. Contains descriptions of the staff below the charts.
  • NondesTest_021508092714.pdf

    Presented at the Western Metals Congress, Los Angeles, California, 15 March 1967.; Archive copy is a photocopy.; ABSTRACT: This report describes the various nondestructive test methods employed to evaluate materials and processes used in the manufacture of large liquid propellant rocket engines at the Rocketdyne Division of North American Aviation, Inc. The contents of the paper were purposely oriented for an audience of aerospace, design and materials engineers. A brief description of liquid propellant rocket engine reliability is presented. The relationship of standards and specifications to nondestructive testing is discussed and various test methods are described along with a discussion of their applications and limitations. The sequence of events leading up to the use of nondestructive testing in production inspection is presented. Finally, the organization of labor directly related to nondestructive testing is given.
  • NoisReduStudScalModeAcouTestFaci_072508164059.pdf

    The acoustic properties of five insulation materials were investigated in a 1/10- scale model acoustic facility. The materials were designed for applications in space vehicles. The model facility, consisting of a reverberation chamber coupled to an anechoic chamber, was evaluated for its use in noise reduction testing. It was found that a reasonably diffuse sound field existed above 900 Hertz. Modal density graphs of the reverberation chamber and spatial acoustic gradients measured within the chamber and across the test panel opening are compared to an idealized facility.; Prepared for the 75th Meeting of the Acoustical Society of America,Ottawa, Ontario, Canada. May 21 - 24, 1968.
  • nextstopthemoon_030209161111.pdf

    Release describing the launch of the Apollo 11.
  • Nextdecainspac_092910155610.pdf

    Summary of President's Advisory Committee report to the President's Space Task Group.
  • newsrocketdyne_062907104301.pdf

    Press release exploring the rockets and projects of the Saturn project.
  • newsreleaseliqhydrog_041207113432.pdf

    Press release covering the nature and use of liquid hydrogen
  • Personneladmin_081808150533.pdf

    Presented at the Society for Personnel Administration. Discusses the problems with the current administration.
  • Persarepobibl_111810115549.pdf

    List of unclassified reports.
  • pdf_043008093902.pdf

    The flrst flight test of the Apollo/Saturn V space vehicle is scheduled for launch from the Natlonal Aeronautics and Space Administration's John F, Kennedy Space Center, Fla., no earlier than Nov. 7. The mission is designated Apollo 4.
  • pdf_041808164234.pdf

    Project indexes included for: Advanced Systems Office, Aero-Astrodynamics Laboratory, Astrionics Laboratory, Computation Laboratory, Engineering Computation Division, Manufacturing Engineering Laboratory, Propulsion and Vehicle Engineering Laboratory, Quality and Reliability Assurance Laboratory, Research and Development Operations, Research Projects Laboratory, and Test Laboratory.
  • pdf_041008090254.pdf

    Includes: Projects Office; Advanced Studies Office; Aerospace Environment Division; Astrodynamics and Guidance Theory Division; Aerophysics Division; Dynamics and Fight Mechanics Division; Flight Test Division.
  • pdf_040108104245.pdf

    This report represents the consolidated instrumentation plan for employing optical and electronic data acquisition systems to monitor the performance and trajectory of the Apollo/Saturn 1B vehicle, AS-2 04/LM-1, during powered flight. Telemetry and electronic tracking equipment on board the vehicle, and data acquisition systems monitoring the flight are discussed. Flight safety instrumentation and vehicle data transmission are described, and geophysical information is provided. This plan reflects the general instrumentation coverage requirements set forth in the NASA Program Support Requirements Document (PSRD) for Apollo/Saturn 16, and the commitments of Eastern Test Range (ETR) Operations Directive (OD) No. 4206,dated 15 August 1967. This plan is not intended to conflict with or to supersede either document. The information presented in this document reflects planning concepts developed prior to October 1, 1967.
  • pdf_032608082835.pdf
  • pdf_013108114114.pdf

    Presented to ACHEMA Congress and European Meeting of Chemical Engineering 1967, Frankfurt, Germany, June 21, 1967 by Dr. Eberhard Rees.; Includes slide numbers.
  • Paylintespacexpe_092607134251.pdf

    Space experimentation requires an increasingly complex planning and systems engineering effort to meet the demand for highest precision and reliability of all measurements and observations. A companion paper discusses the interfaces between the scientific/technical areas of space experimentation and the instruments, subsystems and support systems within the spacecraft. This paper deals with the organization and the procedures which are needed to perform the difficult payload integration process for space experimentation. In the course of this process it is necessary to define the experiments completely, to describe all instruments in terms of engineering specifications, to investigate the commonality of equipment, to group the experiments into mission compatible payloads, to specify acceptable loads on all subsystems and astronauts (when present) and to plan for all contingencies during the flight.
  • partanalprog_062507170113.pdf

    Includes carbon copy of letter sent to David L. Christensen from Ernst Lange regarding the Part Analysis program.
  • Origdrawredpdf_022107152056.pdf

    The document is a photocopy of the Drawing Number Assignments from August 1947 to May 1953. Categories include but are not limited to the drawing number, title, designer, and date finished. Inscribed on the front is "original book property of Jay Laue, MSFC."
  • Orgstrucandmisofaeroendiv_081908151359.pdf

    This document offers a brief description of the Aerospace Environment Division including the basic mission; branches; an organizational directory; and responsibilities of the Environment Research Office, the Atmospheric Dynamics Branch, the Terrestrial Environment Branch, and the Space Environment Branch. William W. Vaughan's name is inscribed on the front page.
  • orgprogandactofthetechsectnorthunt_072208161618.pdf

    This brochure is intended to depict the present status of the technical activities of Nortronics-Huntsville as of the date indicated. It is based on all currently available information. It is subject to periodic revision as additional pertinent information becomes available.
  • orgofacou_060508114422.pdf

    The Organization of a Countdown was developed over 8 years of missiles and space systems testing at the Douglas Aircraft Company, Sacramento test Center. The experience on which this study was based includes the Thor development and acceptance testing, Titan I second stage engine development testing, Development of liquid hydrogen handling techniques, Saturn S-IV and S-IVB development and acceptance testing. The intent of this paper is to examine the static test countdown organization and discuss the need for a systematic method to organize a countdown.
  • Orgacharofthe_091211205523.pdf
  • Orgacharforrock_041508153642.pdf

    Chart No. 1 Rocketdyne master approved by S. K. Hoffman, President (Vice President, North American Aviation, Inc.,).; Chart No. 6.1 Engineering Field Laboratories approved by R. J. Lodge, Director.; Chart No. 6.1.1 Santa Susana Field Laboratory, approved by D. M. Carpenter, Manager.; Chart No. 6.1.2 Field Laboratories Nevada Field Laboratory approved by G. J. Wunderlin, Manager.; Chart No. 6.1.3 Edwards Field Laboratory approved by F. F. Twight, Manager.; Chart No. 6.6 Engineering Administration approved by P. J. Kanne, manager.; Chart No. 12 Solid Rocket Division approved by T. E. Myers.
  • orbreslab_071807093833.pdf

    This report presents the results of the study of Orbiting Research Laboratory and Logistic Spacecraft Checkout Requirements as they relate to prelaunch operations at MILA. The study was performed jointly by the Florida Division and the Systems Research and Analysis Division of TRW Space Technology Laboratories for NASA under the terms of contract NAS10-1076.
  • oppeurpaylsatveh_071907142613.pdf

    Prepared for presentation to the Eurospace Conference. In this paper, we will not deal with the first two questions, which must be of interest to every potential experimenter, but only with the last question of vehicle availability.
  • Operexpesatu_012309125536.pdf

    This paper presents a light, but reverent, discussion of some of the Douglas operational experiences on the Saturn V/S-IVB stage. Certain relevant aspects of earlier work on the Thor intermediate range ballistic missile, the Saturn I S-IV stage, and the Uprated Saturn I S-IVB stage are also discussed.; Aeronautic and Space Engineering and Manufacturing Meeting, Los Angeles, Calif., Oct. 7 - 11, 1968.
  • omsfvolVIIbk2_081707160711.pdf
  • omsfvol7book6_080307101706.pdf
  • omsfvol7book4_080607124403.pdf
  • omsfvol7book3_080307104800.pdf
  • Projapol9nasa.pdf

    Press release surrounding the Apollo 9 rocket and its crew prior to launch.
  • proincrypumdesforspaapp_031808115456.pdf

    Report detailing the problems surrounding cryogenic pump design for space travel and missions.
  • progschemanu_042007183150.pdf

    Manual centered around teaching program schedueling.
  • Progplaneart_012709164341.pdf

    Manned space flight offers the opportunity to couple the astronaut/scientist's ability to select and process data and to calibrate, modify and repair instruments with the vantage point for astronomical observations provided by a platform located above the Earth's atmosphere. This paper briefly examines the role which manned space flight may play in the 1970-1990 time period in meeting astronomy research needs. The instruments and facilities which appear feasible for that period are described.; Paper presented by J. R. Olivier, National Aeronautics and Space Administration, George C. Marshall Space Flight Center and H. L. Wolbers, Ph.D, McDonnell Douglas Astronautics Company - Western Division, Advance Space and Launch Systems.
  • ProgPlanCont_073108102003.pdf

    Saturn S-II Program organizational chart of 1968.
  • Procprogmarsspac_011509113157.pdf

    "Speech presented by Col. John R. McCombs regarding administrative conduct and how they should handle contracts.
  • Probexperprogmane_112707121415.pdf

    Letter to "management" detailing problems identified in management's handling of projects.
  • probassolargscal_062007152941.pdf

    Paper detailing the problems identfified in high pressure testing.
  • Primtheusmann_051410131715.pdf

    Exerpt from George E. Mueller giving a statement to Congress.
  • presrelsatsivfirstfiring_041207105422.pdf

    Following is text of Douglas release on successful first firing of clustered P&W RL10 engines. Occurred at 11:12 A.M. PDT, August 17. Santa Monica, California.; "Sacramento, Calif,--Man's effort to reach the moon moved nearer reality today with the successful first firing here of the six liquid oxygen-liquid hydrogen fueled engines of the Saturn S-IV.
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